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Titanium Alloy Preforms from Plasma Arc Directed Energy Deposition Additive Manufacturing on Substrate, Ti-6Al-4V, Stress Relieved
- Aerospace Material Specification
- AMS7004
- Current
This specification covers preforms fabricated up through 5.5 inches (140 mm) inclusive in deposition width thickness (see 8.2.5) using a Plasma Arc Directed Energy Deposition (PA-DED) additive manufacturing process on a Ti-6Al-4V substrate that are subjected to post-deposition stress relief heat treatment. This is a wire fed additive manufacturing process. If required by the CEO, preforms may require subsequent machining to meet requirements for their intended final part application.
Wire Fed Plasma Arc Directed Energy Deposition Additive Manufacturing Process
- Aerospace Material Specification
- AMS7005
- Current
This specification establishes process controls for the repeatable production of preforms by Wire Fed Plasma Arc Directed Energy Deposition (PA-DED). It is intended to be used for aerospace parts manufactured using Additive Manufacturing (AM) metal alloys, but usage is not limited to such applications.
Nickel Alloy, Corrosion and Heat-Resistant, Powder for Additive Manufacturing, 60Ni - 22Cr - 2.0Mo - 14W - 0.35Al - 0.03La
- Aerospace Material Specification
- AMS7013
- Current
Laser Powder Bed Fusion Process
- Aerospace Material Specification
- AMS7003
- Current
Process Requirements for Production of Metal Powder Feedstock for Use in Additive Manufacturing of Aerospace Parts
- Aerospace Material Specification
- AMS7002
- Current
Laser-Powder Bed Fusion (L-PBF) Produced Parts, Nickel Alloy, Corrosion and Heat-Resistant, 62Ni - 21.5Cr - 9.0Mo - 3.65Nb Stress Relieved, Hot Isostatic Pressed and Solution Annealed
- Aerospace Material Specification
- AMS7000
- Current
Nickel Alloy, Corrosion and Heat-Resistant, Powder for Additive Manufacturing, 62Ni - 21.5Cr - 9.0Mo - 3.65Nb
- Aerospace Material Specification
- AMS7001
- Current
Titanium Alloy Direct Deposited Products 6Al - 4V Annealed
- Aerospace Material Specification
- AMS4999A
- Current
Titanium Alloy Laser Deposited Products 6Al - 4V Annealed
- Aerospace Material Specification
- AMS4999
- Historical